The invention discloses an air landing system of a fixed-wing unmanned aerial vehicle, which belongs to the technical field of aviation and comprises a mother aircraft constructed into a single-wing fixed-wing aircraft, a landing flat plate is arranged above the body of the mother aircraft, and the bottom surface of the landing flat plate is connected with the body of the mother aircraft through a plurality of supporting rods; the landing flat plate is in a horizontal state when the master aircraft is in a level flight state; a friction structure used for increasing friction force is arranged on the top face of the landing flat plate, and a landing mark used for indicating a landing point to the fixed-wing unmanned aerial vehicle is further arranged on the top face of the landing flat plate. The device is simple in structure and reasonable in design, the ship-borne landing process of the fixed-wing unmanned aerial vehicle can be effectively simulated, and related technical verification is facilitated.

    本发明公开了一种固定翼无人机空中着陆系统,属于航空技术领域,包括被构造成下单翼固定翼飞机的母机,母机的机身上方设置有着陆平板,着陆平板的底面通过若干个撑杆与母机的机身相连接,且着陆平板在母机处于平飞状态下时呈水平状;着陆平板的顶面设置有用于增加摩擦力的摩擦结构,着陆平板的顶面还设置有用于向固定翼无人机指示着陆点的着陆标识。本发明结构简单且设计合理,能够有效模拟固定翼无人机舰载着陆过程,以便于进行相关的技术验证。


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    Titel :

    Fixed-wing unmanned aerial vehicle air landing system


    Weitere Titelangaben:

    一种固定翼无人机空中着陆系统


    Beteiligte:
    GONG BANGMIN (Autor:in) / AI JIANLIANG (Autor:in)

    Erscheinungsdatum :

    2022-07-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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